CN103261499B - 用于具有一个或多个拱形部分的由复合材料制成的零件的纤维结构 - Google Patents

用于具有一个或多个拱形部分的由复合材料制成的零件的纤维结构 Download PDF

Info

Publication number
CN103261499B
CN103261499B CN201180059797.7A CN201180059797A CN103261499B CN 103261499 B CN103261499 B CN 103261499B CN 201180059797 A CN201180059797 A CN 201180059797A CN 103261499 B CN103261499 B CN 103261499B
Authority
CN
China
Prior art keywords
fibre structure
composite material
warp
arcuate part
warp thread
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201180059797.7A
Other languages
English (en)
Chinese (zh)
Other versions
CN103261499A (zh
Inventor
蒂里·戈登
布鲁诺·杰克斯·杰拉德·达米布瑞恩
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SNECMA SAS filed Critical SNECMA SAS
Publication of CN103261499A publication Critical patent/CN103261499A/zh
Application granted granted Critical
Publication of CN103261499B publication Critical patent/CN103261499B/zh
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00—Making preforms
    • B29B11/14—Making preforms characterised by structure or composition
    • B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two-dimensional [2D] structure
    • B29C70/222—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two-dimensional [2D] structure the structure being shaped to form a three dimensional configuration
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D1/00—Woven fabrics designed to make specified articles
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D11/00—Double or multi-ply fabrics not otherwise provided for
    • D03D11/02—Fabrics formed with pockets, tubes, loops, folds, tucks or flaps
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D13/00—Woven fabrics characterised by the special disposition of the warp or weft threads, e.g. with curved weft threads, with discontinuous warp threads, with diagonal warp or weft
    • D03D13/004—Woven fabrics characterised by the special disposition of the warp or weft threads, e.g. with curved weft threads, with discontinuous warp threads, with diagonal warp or weft with weave pattern being non-standard or providing special effects
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D25/00—Woven fabrics not otherwise provided for
    • D03D25/005—Three-dimensional woven fabrics
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • D—TEXTILES; PAPER
    • D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2505/00—Industrial
    • D10B2505/02—Reinforcing materials; Prepregs
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24612—Composite web or sheet

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • General Engineering & Computer Science (AREA)
  • Woven Fabrics (AREA)
  • Moulding By Coating Moulds (AREA)
CN201180059797.7A 2010-12-13 2011-12-05 用于具有一个或多个拱形部分的由复合材料制成的零件的纤维结构 Active CN103261499B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1060408 2010-12-13
FR1060408A FR2968679B1 (fr) 2010-12-13 2010-12-13 Structure fibreuse pour piece en materiau composite ayant une ou plusieurs parties en forme d'arche
PCT/FR2011/052868 WO2012080617A1 (fr) 2010-12-13 2011-12-05 Structure fibreuse pour piece en materiau composite ayant une ou plusieurs parties en forme d'arche

Publications (2)

Publication Number Publication Date
CN103261499A CN103261499A (zh) 2013-08-21
CN103261499B true CN103261499B (zh) 2014-12-31

Family

ID=43821920

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201180059797.7A Active CN103261499B (zh) 2010-12-13 2011-12-05 用于具有一个或多个拱形部分的由复合材料制成的零件的纤维结构

Country Status (9)

Country Link
US (1) US9365956B2 (https=)
EP (1) EP2652185B1 (https=)
JP (1) JP6017445B2 (https=)
CN (1) CN103261499B (https=)
BR (1) BR112013014578B1 (https=)
CA (1) CA2820415C (https=)
FR (1) FR2968679B1 (https=)
RU (1) RU2578996C2 (https=)
WO (1) WO2012080617A1 (https=)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2970715B1 (fr) * 2011-01-21 2014-10-17 Snecma Structure fibreuse tissee multicouches ayant une partie tubulaire creuse, procede de fabrication et piece composite la comportant
US9833930B2 (en) 2012-10-23 2017-12-05 Albany Engineered Composites, Inc. Circumferential stiffeners for composite fancases
FR3002548A1 (fr) * 2013-02-22 2014-08-29 Aircelle Sa Procede de tissage d’un tissu en relief, metier a tisser pour realiser le procede et preforme utilisant un tel tissu en relief
FR3002547B1 (fr) * 2013-02-22 2015-07-17 Aircelle Sa Procede de tissage d’un tissu double creneau dans le sens chaine et preforme utilisant un tel tissu.
FR3002549B1 (fr) * 2013-02-22 2015-03-27 Aircelle Sa Metier a tisser a avance multiple, procede de tissage utilisant un tel metier a tisser et un tissu creneau ainsi obtenu.
CA2897519A1 (en) * 2013-03-13 2014-10-09 Aaron D. SIPPEL Compliant composite component and method of manufacture
FR3009315B1 (fr) * 2013-07-30 2015-12-18 Aircelle Sa Procede de fabrication d'une preforme tissee pour une poutre en materiaux composites disposant de renforts interieurs transversaux
FR3018286B1 (fr) * 2014-03-10 2016-05-27 Aircelle Sa Preforme tissee pour realiser un renfort circonferentiel ou torique a section en omega
CN104264312B (zh) * 2014-09-10 2016-04-13 淄博银仕来纺织有限公司 宽幅管状织物的织造方法
FR3027549B1 (fr) * 2014-10-23 2017-09-08 Snecma Assemblage par un element d'ancrage mecanique entre deux pieces dont l'une est realisee en materiau composite
CN107002320B (zh) * 2014-12-10 2018-11-09 内野株式会社 多层纱的制造方法和多层纱织品
JP6377568B2 (ja) * 2015-04-27 2018-08-22 株式会社オルセン 立体織物
FR3065231B1 (fr) * 2017-04-12 2020-03-27 Chamatex Tissu integrant au moins un element de liage
CN110997816B (zh) * 2017-07-31 2022-08-23 美国陶氏有机硅公司 双重可固化有机硅组合物
JP7337051B2 (ja) 2017-10-12 2023-09-01 アルバニー エンジニアード コンポジッツ インコーポレイテッド オメガ形状補強材の三次元織物プリフォーム
US20190285028A1 (en) * 2018-03-16 2019-09-19 Mra Systems, Llc. Thrust reverser cascade
JP6564971B2 (ja) * 2018-03-27 2019-08-28 株式会社オルセン 立体織物を用いた留付具およびこの留付具を用いたテント等の設営方法
FR3084088B1 (fr) * 2018-07-23 2020-10-02 Safran Texture fibreuse pour carter en materiau composite a resistance a l'impact amelioree
FR3092034B1 (fr) * 2019-01-30 2022-12-02 Safran Aircraft Engines Carter en matériau composite avec variation locale d’épaisseur
FR3120878B1 (fr) * 2021-03-17 2023-03-31 Safran Procédé de fabrication d’une pièce de turbomachine en matériau composite comportant une zone de rigidification
FR3136189B1 (fr) * 2022-06-02 2025-04-25 Safran Aircraft Engines Pièce en matériau composite à capacité d’absorption des chocs améliorée, et procédé de fabrication d’une telle pièce

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0391745A1 (en) * 1989-04-06 1990-10-10 Bp Chemicals ( Hitco) Inc. Integrally woven multi-apertured multi-layer angle interlock fabrics
US5098756A (en) * 1989-01-25 1992-03-24 Henderson Mark P Elastic self-extinguishing strap material
CN1216785A (zh) * 1998-09-28 1999-05-19 天津纺织工学院 多层机织物复合材料及成型模具和方法
US6955192B2 (en) * 2001-02-13 2005-10-18 Nippon Filcon Co., Ltd. Vehicle running assisting fabric
FR2904167A1 (fr) * 2006-07-21 2008-01-25 Laudren Electronique Sarl Procede et dispositif de suppression d'echo dans un systeme de communication par digits
CN101473078A (zh) * 2006-06-21 2009-07-01 斯奈克玛动力部件公司 用于复合材料部件的具有复缎编织的增强纤维结构
CN101473079A (zh) * 2006-06-21 2009-07-01 斯奈克玛动力部件公司 用于制造复合材料部件的纤维增强结构
FR2939129A1 (fr) * 2008-11-28 2010-06-04 Snecma Propulsion Solide Aube de turbomachine en materiau composite et procede pour sa fabrication.

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6297938A (ja) * 1985-10-23 1987-05-07 敷島カンバス株式会社 立体成形用織物の製織方法
JPH0243893Y2 (https=) * 1986-07-23 1990-11-21
EP0286004B1 (en) * 1987-03-31 1992-07-22 Asahi Kasei Kogyo Kabushiki Kaisha Woven fabric having multi-layer structure and composite material comprising the woven fabric
EP0481772B1 (en) * 1990-10-18 1996-08-28 Nippon Oil Company, Limited Tubular multilayer woven fabric and method for manufacturing the same
JPH05230735A (ja) * 1992-02-17 1993-09-07 Fukukou Orimono Kk 織物及びその製造方法
RU2117736C1 (ru) * 1997-01-23 1998-08-20 Акционерное общество закрытого типа "Русстек" Волокнистая основа для композиционного изоляционного и/или кровельного материала
FR2759096B1 (fr) * 1997-02-04 1999-02-26 Snecma Texture multicouche liee pour materiaux composites structuraux
FR2887601B1 (fr) 2005-06-24 2007-10-05 Snecma Moteurs Sa Piece mecanique et procede de fabrication d'une telle piece
FR2940167B1 (fr) 2008-12-24 2012-12-21 Messier Dowty Sa Procede de liaison d'un element structurel en materiau composite a un tube.

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5098756A (en) * 1989-01-25 1992-03-24 Henderson Mark P Elastic self-extinguishing strap material
EP0391745A1 (en) * 1989-04-06 1990-10-10 Bp Chemicals ( Hitco) Inc. Integrally woven multi-apertured multi-layer angle interlock fabrics
CN1216785A (zh) * 1998-09-28 1999-05-19 天津纺织工学院 多层机织物复合材料及成型模具和方法
US6955192B2 (en) * 2001-02-13 2005-10-18 Nippon Filcon Co., Ltd. Vehicle running assisting fabric
CN101473078A (zh) * 2006-06-21 2009-07-01 斯奈克玛动力部件公司 用于复合材料部件的具有复缎编织的增强纤维结构
CN101473079A (zh) * 2006-06-21 2009-07-01 斯奈克玛动力部件公司 用于制造复合材料部件的纤维增强结构
FR2904167A1 (fr) * 2006-07-21 2008-01-25 Laudren Electronique Sarl Procede et dispositif de suppression d'echo dans un systeme de communication par digits
FR2939129A1 (fr) * 2008-11-28 2010-06-04 Snecma Propulsion Solide Aube de turbomachine en materiau composite et procede pour sa fabrication.

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
JP特开平5-230735A 1993.09.07 *

Also Published As

Publication number Publication date
CA2820415A1 (fr) 2012-06-21
EP2652185B1 (fr) 2015-06-24
EP2652185A1 (fr) 2013-10-23
JP2014506304A (ja) 2014-03-13
BR112013014578B1 (pt) 2020-12-01
CA2820415C (fr) 2018-03-20
US20130270389A1 (en) 2013-10-17
US9365956B2 (en) 2016-06-14
CN103261499A (zh) 2013-08-21
RU2013132219A (ru) 2015-01-20
JP6017445B2 (ja) 2016-11-02
BR112013014578A2 (pt) 2016-09-20
RU2578996C2 (ru) 2016-03-27
FR2968679B1 (fr) 2014-02-07
WO2012080617A1 (fr) 2012-06-21
FR2968679A1 (fr) 2012-06-15

Similar Documents

Publication Publication Date Title
CN103261499B (zh) 用于具有一个或多个拱形部分的由复合材料制成的零件的纤维结构
CN102666277B (zh) 航空器螺旋桨叶片以及叶片的制造方法
CN105358429B (zh) 用于飞行器的复合螺旋桨叶片
CN103415388B (zh) 包括固定装置的复合材料零件
JP6734261B2 (ja) 有機マトリックスを伴う複合材料から成る自己補剛ケーシング
JP5913303B2 (ja) 一体型複合けたを有するブレード
JP2014506304A5 (https=)
CN114728440B (zh) 用于制造风扇叶片的由复合材料制成的编织的纤维预成型件
JP6254532B2 (ja) 薄肉部を有する複合材料部品のための繊維補強構造
CN102666050B (zh) 编织预制件、复合材料、及其制造方法
US9382647B2 (en) Fibrous structure for a part made of a composite material and having a complex shape
US11767098B2 (en) Propeller blade or vane for an aircraft with particular weaving of a fibre preform receiving a bladder filled with a shaping foam
JP6092244B2 (ja) 可変量の糸を有する繊維構造体
CN112601849A (zh) 用于由复合材料制备的抗冲击性提高的壳体的纤维织构
CN115003482B (zh) 用于生产复合材料零件、特别是涡轮机叶片的编织纤维预制件
US11890822B2 (en) Component of revolution made of composite material having improved resistance to delamination
CN116134212A (zh) 具有三维编织的纤维增强和二维编织的表层的复合材料制成的叶片及其制造方法
CN112513352A (zh) 用于由复合材料制备的抗剪强度提高的壳体的纤维织构
CN118139740A (zh) 用于制造包括加强腔体的叶片的方法

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant